View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 67731U 26145.41213605 +.00000000 +00000-0 +50737-3 0 00002
2 67731 97.2855 198.9294 0000447 111.4959 248.6332 15.33443397 09
| Epoch (UTC): | 25 May 2026 09:53:28 |
| Eccentricity: | 0.0000447 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 198.9294° |
| argument of perigee: | 111.4959° |
| revolutions per day: | 15.33443397 |
| mean anomaly at epoch: | 248.6332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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